Preparing strength check notes, stress analysis packages, in support of material review dispositions to resolve anomalies created on the production floor during the manufacture of Boeing wing leading edge components.
A temporary need for aircraft structural analysis engineers that can accomplish quick but accurate stress and fatigue checks of existing rejection tag discrepancies. The primary task is to ensure that previously provided stress concurrences are still in accordance with the latest Boeing-provided loads, methods, and allowables.
Note that detailed FEM work, and generation of extensive formal stress reports is not required. Experience in a material review environment is preferred along with a minimum of 10 years in the industry.